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Anthony Bouvette Phones & Addresses

  • 211 Eaton Ave, Hamilton, OH 45013 (616) 443-0919
  • Grand Rapids, MI
  • 211 Eaton Ave, Hamilton, OH 45013

Work

Company: Ge avaition Sep 2011 Position: Lead engineer - emi / hirf / lightning

Education

School / High School: Calvin College- Grand Rapids, MI May 2005 Specialities: Bachelor of Science in Physics

Languages

English

Ranks

Certificate: Inarte, License Emc-003446-Nt

Industries

Aviation & Aerospace

Resumes

Resumes

Anthony Bouvette Photo 1

Lead Engineer, Inlet And Exhaust Rcs Testing And Materials

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Location:
211 Eaton Ave, Hamilton, OH 45013
Industry:
Aviation & Aerospace
Work:
GE Aviation - Cincinnati Area since Sep 2011
Lead Engineer, EMI / Lightning

L-3 Communications Cincinnati Electronics - Cincinnati Area Jul 2009 - Sep 2011
EMI Test Technician

Intertek Testing Services - Greater Grand Rapids, Michigan Area Aug 2005 - Jul 2009
Project Manager / Test Engineer
Education:
Calvin College 2001 - 2005
BS, Physics
Languages:
English
Certifications:
Inarte, License Emc-003446-Nt
License Emc-003446-Nt
Anthony Bouvette Photo 2

Anthony Bouvette Hamilton, OH

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Work:
GE Avaition

Sep 2011 to 2000
Lead Engineer - EMI / HIRF / Lightning

L-3 Communications: Cincinnati Electronics
Mason, OH
Jul 2009 to Sep 2011
EMI / EMC Test Engineer

Intertek ETL SEMKO
Grand Rapids, MI
Aug 2005 to Jul 2009
Test Engineer / Project Manager

Education:
Calvin College
Grand Rapids, MI
May 2005
Bachelor of Science in Physics

Publications

Us Patents

Propulsion System For An Aircraft

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US Patent:
20180304753, Oct 25, 2018
Filed:
Apr 21, 2017
Appl. No.:
15/493544
Inventors:
- Schenectady NY, US
Anthony Austin Bouvette - Hamilton OH, US
Glenn David Crabtree - Oregonia OG, US
International Classification:
B60L 11/14
B64D 27/12
B64D 27/18
B64C 21/06
H02G 5/10
F02K 3/04
F02C 6/20
H02K 7/18
Abstract:
A propulsion system for an aircraft includes an electric power source and an electric propulsion assembly having an electric motor and a propulsor, the propulsor powered by the electric motor. The propulsion system also includes an electric power bus electrically connecting the electric power source to the electric propulsion assembly. The electric power source is configured to provide electrical power to the electric power bus, and the electric power bus is configured to transfer the electric power to the electric propulsion assembly at a voltage exceeding 800 volts.

Propulsion System For An Aircraft

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US Patent:
20180305036, Oct 25, 2018
Filed:
Apr 21, 2017
Appl. No.:
15/493623
Inventors:
- Schenectady NY, US
Anthony Austin Bouvette - Hamilton OH, US
Robert Charles Hon - Fort Mitchell KY, US
International Classification:
B64D 33/08
B64D 27/18
B64D 27/24
B64C 21/06
B60L 11/14
F02K 3/04
H02G 5/10
H02K 9/19
H02K 7/18
Abstract:
A propulsion system for an aircraft includes an electric power source, an electric propulsor assembly having an electric motor and a propulsor configured to generate thrust for the aircraft, and a power bus electrically connecting the electric power source to the electric propulsor assembly such that the electric power source powers the electric propulsor assembly. The power bus includes an electric line and a fluid cooling system, the fluid cooling system extending along at least a portion of a length of the electric line. The fluid cooling system is in thermal communication with the electric line for cooling the electric line during operation and is further in thermal communication with the electric motor of the electric propulsor assembly for cooling the electric motor of the electric propulsor assembly.
Anthony Bouvette from Hamilton, OH Get Report